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Computer aided design device for integration performance optimization of airliner and fanjet and method thereof

A turbofan engine, computer-aided technology, applied in the field of aero-engine, can solve the problem that the mutual requirements and influence of technical parameters of aircraft and turbofan engine cannot be considered in coordination.

Inactive Publication Date: 2012-06-13
BEIHANG UNIV
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AI Technical Summary

Problems solved by technology

However, the disadvantage of these design tools is that the engine performance design tool and the aircraft performance design tool are independent of each other, and the mutual requirements and influences of the technical parameters of the aircraft and the turbofan engine cannot be considered together

Method used

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  • Computer aided design device for integration performance optimization of airliner and fanjet and method thereof
  • Computer aided design device for integration performance optimization of airliner and fanjet and method thereof
  • Computer aided design device for integration performance optimization of airliner and fanjet and method thereof

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Embodiment Construction

[0017] The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0018] Such as figure 1 Shown is a structural schematic diagram of a computer-aided design device for optimizing the integrated performance of a passenger plane and a turbofan engine according to the present invention. The CAD device can be a desktop computer or a portable computer, and its basic hardware structure includes an input device 1 , a central processing unit 2 , a memory module 3 , a storage device 4 and a display device 5 .

[0019] The input device 1 is used to input manipulation instructions or related parameters to the central processing unit 2, which includes a keyboard, mouse or other input devices. The central processing unit 2 is used to execute all programs in the memory module 3, the main frequency of the central processing unit 2 is required to be above 1.0G, and the space required by the memory module 3 is at least 256M. The s...

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Abstract

The invention discloses a computer aided design device for the integration performance optimization of an airliner and a fanjet and a method thereof, which belong to the technical field of aerial engines. The design device is characterized in that an input device, a central processing unit, an internal storage module, a storage device and a display device are connected through a data line. The internal storage module comprises a system program library, a system interactive operation window, a fanjet design module, a fanjet size / weight / resistance estimating module, an airliner flying performance simulation module and an airliner / fanjet integration performance optimizing module. The design device and the method can quickly and fully consider mutual requirements and effect of the technical parameter of the airliner and the fanjet, conduct performance matching calculation and evaluation of the existing airliners and the existing engines and performance matching calculation, optimization and evaluation research of the newly designed air liners and engines.

Description

technical field [0001] The invention belongs to the technical field of aero-engines, and in particular relates to a computer-aided design device and method for optimizing the integrated performance of a passenger plane and a turbofan engine. Background technique [0002] At present, the tools for performance design and calculation of gas turbine engines in the published literature at home and abroad include GSP, Turbomach, Gasturb, NPSS and ASP, etc., see reference [1]: MachMillan W.L.Development of a Modular Type Program for the Calculation of Gas Turbine Off-design Performance.Ph.D.Thesis, C.I.T, September, 1974; Reference [2]: Sirinoglou A.Implementation of Variable Geometry for Gas Turbine Performance Simulation Turbomach Improvement.M.Sc.Thesis, C.I.T, September 1992; Reference [3]: Joachim Kurzke, Advanced User-friendly Gas Turbine Performance Calculations on a Personal Computer, ASME 95-GT-147; Reference [4]: ​​Mark G.Turner, John A. Reed, Robert Ryder, Jospeh P.Vere...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCY02T90/00
Inventor 陈敏唐海龙欧阳辉
Owner BEIHANG UNIV
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